ES2244738T3 - Alabe para turbina que comprende un deflector de aire de refrigeracion. - Google Patents
Alabe para turbina que comprende un deflector de aire de refrigeracion.Info
- Publication number
- ES2244738T3 ES2244738T3 ES02290964T ES02290964T ES2244738T3 ES 2244738 T3 ES2244738 T3 ES 2244738T3 ES 02290964 T ES02290964 T ES 02290964T ES 02290964 T ES02290964 T ES 02290964T ES 2244738 T3 ES2244738 T3 ES 2244738T3
- Authority
- ES
- Spain
- Prior art keywords
- blade
- air
- foot
- turbine
- socket
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 238000005057 refrigeration Methods 0.000 title description 4
- 241000535417 Alabes Species 0.000 title 1
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 238000001816 cooling Methods 0.000 claims abstract description 54
- 230000005465 channeling Effects 0.000 claims description 4
- 238000011144 upstream manufacturing Methods 0.000 description 4
- 210000000078 claw Anatomy 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 210000003456 pulmonary alveoli Anatomy 0.000 description 2
- 230000000284 resting effect Effects 0.000 description 2
- 238000007789 sealing Methods 0.000 description 2
- 238000005219 brazing Methods 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000037213 diet Effects 0.000 description 1
- 235000005911 diet Nutrition 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0105289 | 2001-04-19 | ||
| FR0105289A FR2823794B1 (fr) | 2001-04-19 | 2001-04-19 | Aube rapportee et refroidie pour turbine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES2244738T3 true ES2244738T3 (es) | 2005-12-16 |
Family
ID=8862464
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES02290964T Expired - Lifetime ES2244738T3 (es) | 2001-04-19 | 2002-04-17 | Alabe para turbina que comprende un deflector de aire de refrigeracion. |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US6981845B2 (fr) |
| EP (1) | EP1251243B8 (fr) |
| JP (1) | JP4112986B2 (fr) |
| CA (1) | CA2444862C (fr) |
| DE (1) | DE60205977T2 (fr) |
| ES (1) | ES2244738T3 (fr) |
| FR (1) | FR2823794B1 (fr) |
| RU (1) | RU2325537C2 (fr) |
| UA (1) | UA73655C2 (fr) |
| WO (1) | WO2002086291A1 (fr) |
Families Citing this family (34)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB0227745D0 (en) * | 2002-11-28 | 2003-01-08 | Rolls Royce Plc | Blade cooling |
| US6974306B2 (en) * | 2003-07-28 | 2005-12-13 | Pratt & Whitney Canada Corp. | Blade inlet cooling flow deflector apparatus and method |
| FR2858829B1 (fr) | 2003-08-12 | 2008-03-14 | Snecma Moteurs | Aube refroidie de moteur a turbine a gaz |
| GB0405679D0 (en) * | 2004-03-13 | 2004-04-21 | Rolls Royce Plc | A mounting arrangement for turbine blades |
| EP1730389B1 (fr) * | 2004-03-30 | 2009-12-09 | Alstom Technology Ltd | Dispositif pour alimenter une aube en air de refroidissement |
| US7578652B2 (en) | 2006-10-03 | 2009-08-25 | United Technologies Corporation | Hybrid vapor and film cooled turbine blade |
| SG143087A1 (en) * | 2006-11-21 | 2008-06-27 | Turbine Overhaul Services Pte | Laser fillet welding |
| US20090068446A1 (en) | 2007-04-30 | 2009-03-12 | United Technologies Corporation | Layered structures with integral brazing materials |
| US8128365B2 (en) | 2007-07-09 | 2012-03-06 | Siemens Energy, Inc. | Turbine airfoil cooling system with rotor impingement cooling |
| FR2937372B1 (fr) * | 2008-10-22 | 2010-12-10 | Snecma | Aube de turbine equipee de moyens de reglage de son debit de fluide de refroidissement |
| WO2011026503A1 (fr) | 2009-09-04 | 2011-03-10 | Siemens Aktiengesellschaft | Procédé et dispositif d'orientation tangentielle d'un refroidissement interne sur une aube directrice |
| US8622702B1 (en) * | 2010-04-21 | 2014-01-07 | Florida Turbine Technologies, Inc. | Turbine blade with cooling air inlet holes |
| GB201016597D0 (en) | 2010-10-04 | 2010-11-17 | Rolls Royce Plc | Turbine disc cooling arrangement |
| IT1403416B1 (it) * | 2010-12-21 | 2013-10-17 | Avio Spa | Rotore palettato di una turbina a gas per motori aeronautici e metodo per il raffreddamento di detto rotore palettato |
| DE102011121634B4 (de) * | 2010-12-27 | 2019-08-14 | Ansaldo Energia Ip Uk Limited | Turbinenschaufel |
| US20120315139A1 (en) * | 2011-06-10 | 2012-12-13 | General Electric Company | Cooling flow control members for turbomachine buckets and method |
| EP2639407A1 (fr) | 2012-03-13 | 2013-09-18 | Siemens Aktiengesellschaft | Agencement de turbine à gaz pour diminuer les contraintes sur des disques de turbine et turbine à gaz associée |
| US9435206B2 (en) | 2012-09-11 | 2016-09-06 | General Electric Company | Flow inducer for a gas turbine system |
| EP2725191B1 (fr) * | 2012-10-23 | 2016-03-16 | Alstom Technology Ltd | Turbine à gaz et aube de turbine pour une telle turbine à gaz |
| US8926283B2 (en) * | 2012-11-29 | 2015-01-06 | Siemens Aktiengesellschaft | Turbine blade angel wing with pumping features |
| US20160090841A1 (en) * | 2014-09-29 | 2016-03-31 | United Technologies Corporation | Gas turbine engine blade slot heat shield |
| US10094228B2 (en) * | 2015-05-01 | 2018-10-09 | General Electric Company | Turbine dovetail slot heat shield |
| CN107849925B (zh) * | 2015-07-06 | 2020-03-17 | 西门子股份公司 | 具有冷却流量调节特征的涡轮机定子叶片和/或涡轮机转子叶片以及适应叶片的对应方法 |
| DE102015111746A1 (de) * | 2015-07-20 | 2017-01-26 | Rolls-Royce Deutschland Ltd & Co Kg | Gekühltes Turbinenlaufrad, insbesondere für ein Flugtriebwerk |
| GB201516657D0 (en) | 2015-09-21 | 2015-11-04 | Rolls Royce Plc | Seal-plate anti-rotation in a stage of a gas turbine engine |
| US20170234447A1 (en) * | 2016-02-12 | 2017-08-17 | United Technologies Corporation | Methods and systems for modulating airflow |
| KR102025147B1 (ko) * | 2017-10-13 | 2019-09-27 | 두산중공업 주식회사 | 버킷의 쓰로틀 플레이트 결합구조와 이를 포함하는 회전체 및 가스터빈 |
| DE102019206432A1 (de) * | 2019-05-06 | 2020-11-12 | MTU Aero Engines AG | Turbomaschinenschaufel |
| KR102284507B1 (ko) * | 2020-02-25 | 2021-08-02 | 두산중공업 주식회사 | 로터 및 이를 포함하는 터보머신 |
| US11560844B2 (en) * | 2021-02-18 | 2023-01-24 | Pratt & Whitney Canada Corp. | Inertial particle separator for a turbine section of a gas turbine engine |
| US12398644B2 (en) * | 2022-07-08 | 2025-08-26 | Siemens Energy Global GmbH & Co. KG | Manifold for turbine blade of gas turbine engine |
| US12110809B1 (en) | 2023-04-04 | 2024-10-08 | Ge Infrastructure Technology Llc | Turbine blade and assembly with dovetail arrangement for enlarged rotor groove |
| US12018590B1 (en) | 2023-04-04 | 2024-06-25 | Ge Infrastructure Technology Llc | Method for turbine blade and assembly with dovetail arrangement for enlarged rotor groove |
| US12410712B1 (en) | 2024-09-24 | 2025-09-09 | Pratt & Whitney Canada Corp. | Rotor blade with apertured cooling air deflector |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB742477A (en) * | 1952-10-31 | 1955-12-30 | Rolls Royce | Improvements in or relating to bladed stator or rotor constructions for fluid machines such as axial-flow turbines or compressors |
| GB1605282A (en) * | 1973-10-27 | 1987-12-23 | Rolls Royce 1971 Ltd | Bladed rotor for gas turbine engine |
| GB1561229A (en) * | 1977-02-18 | 1980-02-13 | Rolls Royce | Gas turbine engine cooling system |
| DE2941866C2 (de) * | 1978-10-26 | 1982-08-19 | Rolls-Royce Ltd., London | Turbine für ein Gasturbinentriebwerk mit lufgekühlten Turbinenschaufeln |
| US4626169A (en) * | 1983-12-13 | 1986-12-02 | United Technologies Corporation | Seal means for a blade attachment slot of a rotor assembly |
| SU1287678A2 (ru) * | 1984-09-11 | 1997-02-20 | О.С. Чернилевский | Охлаждаемая лопатка турбины |
| SU1369390A1 (ru) * | 1986-06-02 | 1996-12-20 | Уфимский авиационный институт им.Серго Орджоникидзе | Устройство для охлаждения рабочих лопаток газовой турбины |
| US4820123A (en) * | 1988-04-25 | 1989-04-11 | United Technologies Corporation | Dirt removal means for air cooled blades |
| DE3835932A1 (de) * | 1988-10-21 | 1990-04-26 | Mtu Muenchen Gmbh | Vorrichtung zur kuehlluftzufuehrung fuer gasturbinen-rotorschaufeln |
| US5403156A (en) * | 1993-10-26 | 1995-04-04 | United Technologies Corporation | Integral meter plate for turbine blade and method |
| US6059529A (en) * | 1998-03-16 | 2000-05-09 | Siemens Westinghouse Power Corporation | Turbine blade assembly with cooling air handling device |
-
2001
- 2001-04-19 FR FR0105289A patent/FR2823794B1/fr not_active Expired - Lifetime
-
2002
- 2002-04-17 WO PCT/FR2002/001325 patent/WO2002086291A1/fr not_active Ceased
- 2002-04-17 JP JP2002583793A patent/JP4112986B2/ja not_active Expired - Fee Related
- 2002-04-17 US US10/474,038 patent/US6981845B2/en not_active Expired - Lifetime
- 2002-04-17 UA UA2003109399A patent/UA73655C2/uk unknown
- 2002-04-17 ES ES02290964T patent/ES2244738T3/es not_active Expired - Lifetime
- 2002-04-17 DE DE60205977T patent/DE60205977T2/de not_active Expired - Lifetime
- 2002-04-17 CA CA002444862A patent/CA2444862C/fr not_active Expired - Fee Related
- 2002-04-17 EP EP02290964A patent/EP1251243B8/fr not_active Expired - Lifetime
- 2002-04-17 RU RU2003133669/06A patent/RU2325537C2/ru not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| DE60205977D1 (de) | 2005-10-13 |
| EP1251243A1 (fr) | 2002-10-23 |
| JP4112986B2 (ja) | 2008-07-02 |
| JP2004522049A (ja) | 2004-07-22 |
| FR2823794B1 (fr) | 2003-07-11 |
| EP1251243B8 (fr) | 2005-11-02 |
| UA73655C2 (uk) | 2005-08-15 |
| EP1251243B1 (fr) | 2005-09-07 |
| US20040115054A1 (en) | 2004-06-17 |
| RU2325537C2 (ru) | 2008-05-27 |
| CA2444862C (fr) | 2009-11-24 |
| CA2444862A1 (fr) | 2002-10-31 |
| RU2003133669A (ru) | 2005-04-20 |
| DE60205977T2 (de) | 2006-07-06 |
| US6981845B2 (en) | 2006-01-03 |
| FR2823794A1 (fr) | 2002-10-25 |
| WO2002086291A1 (fr) | 2002-10-31 |
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